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塞斯纳172飞行员操作手册 Cessna 172 PILOT'S OPERATING HANDBOOK(57)

时间:2011-12-29 11:03来源:蓝天飞行翻译 作者:航空 点击:

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Total the weights and moments/ 1000 and plot these values on the Center of Gravity Moment Envelope to determine whether the point falls within the envelope, and if the loading is acceptable.
 
Figure 6-3. Loading Arrangements
 

Moment
(lb. - ins.
/1000)         8. Locate this point (2300 at 103.2) on the Center of Gravity Moment Envelope,
and since this point falls within the envelope, the loading is acceptable.
NOTE
* The maximum allowable combined weight capacity for baggage areas 1 and 2 is 120 lbs.
          
SAMPLE AIRPLANE Moment
(lb. -ins.
/1000) (0.
r-• in  9Z I. 12.4 .-
a)  1 103.2 
 Weight
(lbs.)  CNI   cro
co c) N.
.- cn
cr)  2300 
SAMPLE
LOADING PROBLEM 1. Basic Empty Weight (Use the data pertaining to your airplane as it is presently equipped. Includes unusable
fuel and full oil)  
2. Usable Fuel (At 6 Lbs./Gal.)
Standard Tanks (40 Gal. Maximum)  
Long Range Tanks (50 Gal. Maximum)  
3. Pilot and Front Passenger (Station 34 to 46)  
4. Rear Passengers  
5. * Baggage Area 1 or Passenger on Child's Seat
(Station 82 to 108) 120 Lbs. Max.  
6. * Baggage Area 2 (Station 108 to 142) 50 Lbs. Kix   7. TOTAL WEIGHT AND MOMENT 
 

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LO
N Lon LO
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S g S g S
r-.

 
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